Broadband Liner Optimization for the Source Diagnostic Test Fan-Reference-Cited by-同舟云学术

Broadband Liner Optimization for the Source Diagnostic Test Fan

Published:2012-06-04 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
language:
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Author:

Nark Douglas¹,Jones Michael¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2195

Reference19 articles.

1. 1Schuster,B.,Lieber,L.,andVavalle,A.“OptimziationofaSeamlessInletLinerUsinganEmpiricallyValidatedPredictionMethod,”AIAA Paper2010-3824,2010.

2. 2Weir,D.“EngineValidationofNoiseandEmissionReductionTechnologyPhaseI,”NASACR2008-215225,2008.

3. 3Nark,D.M.“AssessmentofRadiatedFanNoisePredictionCapabilitiesusingStaticEngineTestData,”AIAAPaper2011-2807,2011.

4. 4Jones, M. G., Howerton, B. M., and Ayle, E. “Evaluation of Parallel-Element, Variable-Impedance, Broadband Acoustic Liner Concepts,” 18thAIAA/CEASAeroacousticsConference,AmericanInstituteofAeronauticsandAstronautics,Reston,VA(submittedforpublication).

5. 5Hughes,C.E.“AerodynamicPerformanceofScale-ModelTurbofanOutletGuideVanesDesignedforLowNoise,”AIAAPaper2002-0374, 2002.

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